Concentric Wing Turbines

ABSTRACT

A harnessing module for harnessing renewable wind and water energy comprises opposing concentric wings for rotation about a shaft having a hub comprising at least one pair of opposing concentric wings for use in generating renewable electrical energy. Each concentric wing of the opposing concentric wings may have a circular leading edge for facing one of air and water flow, each concentric wing having a generally curved upper surface but for a curved downward surface and a sharp trailing edge opposite the circular leading edge of each concentric wing. The circular side and curved upper surface are preferably at a positive angle of attack where one of water or wind flow is received at the circular side and provides lifting rotation of the opposing concentric wings. Hence, the opposing concentric wings rotate about the turbine shaft and comprise a harnessing module for generating electricity from either the wind or water flow.

This application is a continuation-in-part of U.S. patent application Ser. No. 16/233,365 filed Dec. 27, 2018 and claims the right of priority to U.S. Provisional Patent Application Ser. No. 62/779,683 filed Dec. 14, 2018 by Kyung Soo Han which is a continuation-in-part of U.S. patent application Ser. No. 16/134,595, entitled “River and Tidal Turbine with Power Control,” filed Sep. 18, 2018, by Kyung Soo Han, all priority patent applications being incorporated by reference matter as to their entire contents.

TECHNICAL FIELD

The field of the invention relates to the paddles, blades, propellers, buckets, sails or wings of wind, river, tidal or ocean wave turbines and, more particularly, to one of a pair of concentric wings useful in a wind or river turbine similar to an airplane wing and a pair of concentric, triangular wings having curved leading and trailing edges useful in one of a wind, tidal turbine or a wave turbine for harnessing wind or water energy.

BACKGROUND

There are three components of a turbine: a harnessing module, a controlling module and a generating module. The harnessing module is for harnessing the energy of the wind from the flow of air and energy from the water from river flow, tidal changes, ocean currents, wave motion and other water energy. Medium to high speed wind flow is typically stronger at the top or side of a hill than in a valley. Also, studies show that due to climate change, wind speeds have been increasing in recent years. A paddle, blade, propeller, bucket, sail or wing are used to capture or harness energy of the wind, the river, the ocean or tidal energy of tidal currents and changing tides. Water has a higher density than air and so creates greater torque than the same flow air. The paddle wheel is known to propel a river boat forward and has been used to capture river energy. A propeller/blade has been known to capture wind, river or ocean current energy.

A controlling and generating module and some concepts of a harnessing module are to be found in the following U.S. patent and pending patent applications of Kyung Soo Han which are to be considered incorporated by reference as to their entire contents: U.S. patent application Ser. No. 15/267,655 filed Sep. 16, 2016 issued as U.S. Pat. No. 9,912,209; U.S. Ser. No. 15/707,138 filed Sep. 18, 2017, entitled Commutator-less and Brush-less Direct Current Generator and Applications for Generating Power to an Electric Power System and issued as U.S. Pat. No. 10,378,506; U.S. Ser. No. 15/883,927 filed Jan. 30, 2018 entitled Control Apparatus and Method for Variable Renewable Energy and U.S. Ser. No. 16/134,595 filed Sep. 18, 2018 for River and Tidal Turbine with Power Control. Moreover, U.S. patent application Ser. No. 16/233,365, filed Dec. 27, 2018, should also be considered incorporated by reference as it provides recently developed material directed to the control and generating modules and shows a known harnessing module for harnessing river, tidal and ocean current energy.

It is an object of the present invention to study the application of wings typically used for flight in the form of a wing or blade to determine if such concentric wings may be of interest for forming a harnessing module of a turbine. Applicant has also studied the principles of an airfoil and the possibility of developing fixed wings for harnessing uni-directional river energy and for bi-directional tidal and ocean wave energy.

Problems of prior art harnessing modules include the use of a hatch to control, for example, speed of a waterwheel, the large size and volume of noise generated by known wind turbine propellers and the need to adapt the support structure such as a platform to both support the turbine and the control and generating modules above a river and a harnessing module, for example, below a river turbine complicates the design of a river turbine. A water flow turbine comprises a controlling module and a generating module on top of the platform while permitting a harnessing module to be mounted under the platform. In the alternative, a water flow turbine may be mounted, for example, on a platform secured to a river bottom. A concentric wing turbine (CWT) is an option over existing harnessing modules, for example, paddles, blades, and propellers. Known propellers create thrust for a vehicle such as an airplane or helicopter to move forward or upward/downward through the air. Wings of airplanes in addition to propellers are creating lift for a vehicle/airplane to go forward/upward/downward. A known harnessing module comprises hatches and paddle wheels. There remains a problem in the art that suggests an analogy between the wing or propeller of an aircraft and a harnessing module of a hydrokinetic or wind turbine. A harnessing module should create lift or rotation since the renewable energy flow (wind or water) is providing thrust.

SUMMARY OF THE EMBODIMENTS

A solution to the above-identified problems of developing wings for harnessing modules of variable energy power generators is a Concentric Wing Turbine (CWT). A CWT is a renewable energy harnessing module that consists of rotating wings that may be similar to helicopter rotor blades in multiples of N pairs of wings where N is equal to or greater than one. The purpose of using concentric wings is harnessing high torque at controlled rotational speed with wider and concentrically shaped blades. The term “concentric” as used herein means sharing a common center, for example, a center of mass or geometric center of a triangle. Once rotary energy is harnessed effectively, a speed converter developed by DDMotion can convert the harnessed speed/torque (energy) to grid quality electricity. The primary application of a harnessing module is for harnessing river energy that is flowing in one direction. Since turbines are fixed at a particular location, sometimes by ties to a rivers borders or their bottoms are harnessing rotary energy instead of moving the system (such as an airplane) forward. Creating greater lift and drag is desirable in designing a wing/blade for a uni-directional flow of rotational energy in a harnessing module that may turn an electric generator. Another application is harnessing tidal (bidirectional) energy and wave energy. In this case, the direction of harnessed energy may be adapted to rotate a shaft of a speed converter/controlling module in one direction. With changing tides, it is useful to apply a harnessing module capable of operating in two directions of the changing tides. For example, the East River of New York City changes direction twice a day as do tidal estuaries. Ocean waves exhibit two directional, up and down, movement and water flow. Energy may be harnessed by a similar bi-directional harnessing module adapted to turn a control shaft in one direction.

There are three types of turbines in reference to the flow of energy versus a rotational axis of the harnessing modules. The axis of the rotating shaft of Horizontal Axis Wind Turbines is in-line with the flow, Vertical Axis Wind Turbines and wave turbines are vertical, and a paddle type waterwheel is horizontally perpendicular. Out of the three types, the in-line system is most effective without dead angles. A CWT preferably may have an in-line system. As will be discussed in the brief description of the drawings and the following detailed description, an airplane or helicopter wing has been studied for the purpose of determining modifications of known wings that may be adapted for the use of harnessing river or wind energy that may be input to a controlling module and a generating module for outputting constant power at constant frequency to an electric grid.

BRIEF DESCRIPTION OF THE DRAWINGS

In the drawings, a convention is used where the first number of a reference numeral provides the figure number and an effort is made to use the remaining digits consistently for similar components referenced in subsequent drawings.

FIG. 1A is a front view and FIG. 1B is a side view of a river turbine comprising a generator 155, a control motor 135 and speed converter 145 components mounted on a plate 192 of a platform 150 that may be tied to a river bottom or a river bank (or at least the harnessing module comprising concentric wings 120A-H may be in the water). A problem in cold climates is that a river may freeze in winter months, for example, if located in Canada, and the use of a river turbine mounted on a floating platform 150 in such a cold climate may be limited. Blades 120C and 120G, for example, each form a concentric wing and together an opposing pair of blades surrounding a hub and a shaft 130 where the hub may be circular, oval, square or rectangular. Each blade has a common center that may be geometrically determined and shaft 130 supports the blades at this common center. As will be defined herein, each blade has an axis of attack that is an angle at which the concentric wing receives the uni-directional flow of water (or air). The harnessing module of FIGS. 1A and 1B is identified by blades 120A through 120H tied/attached to a shaft 130. FIG. 1B is a side view of the river turbine of FIG. 1A proposing that a concentric wing 195 be used as a blade 120A through 120H. In FIGS. 1A and 1B, river turbines of the prior art are typically mounted on floating platforms 150 but may be designed with turbine blades that may look like propellers or rotating barrels of blades. It is an object of the present invention to study airplane wings such as concentric wings for the purpose of harnessing greater energy amounts than is known from using paddles, buckets, blades or propeller blades known in the art.

FIGS. 2A and 2B show an example of a harnessing module mounted under floating platform 210. A hatch 220 may be attached to/surrounded by a paddle or vane 240 so that the hatch 220 may be moved by paddle or vane 240 180 degrees from the bottom position shown in FIG. 2A to the opposite top side with water flow from the right to left versus left to right through one side of the harnessing module because of the water flow controlling the location of the paddle or vane 240. The hatch 220 may move to the opposite side to the position shown in FIG. 2B when the water flow changes from left to right to right to left when the paddle of vane 240 catches the water flow from right to left rotating the hatch 220. FIGS. 2A and 2B do not show concentric wings (unlabeled). They show buckets that, for example, in FIG. 2A will capture the water flow from right to left (and FIG. 2B will capture water and rotate when water flow is from left to right. Paddle or vane 240 is free to move about shaft 215 with hatch 220 in whichever direction the water flows.

FIG. 3A shows a front view of a waterwheel having protector bars 310, 320 for protecting the waterwheel (harnessing module) from floating debris. The waterwheel of FIG. 3A may also be used for bi-directional water flow. Waterwheel 340 rotation can be bi-directional and be controlled, for example, with the protector bars 310, 320 stationary and the moveable trap doors 330 moved to an open or closed position depending on the direction of water flow—right to left water flow being shown with a hatch known in the art or trap doors 330.

FIG. 3B shows a side view of a waterwheel with water flowing from right to left. Note that the water flow closes the bottom trap door 330 (at the lower right) and opens the top trap door 330 (at the upper left) when water flows from right to left. So, the top half of the waterwheel is used in FIG. 3B with water flowing from right to left. If water flowed in the opposite left to right direction, the right moveable trap door 330 at the bottom right (the moveable trap door 330 at top left close) would be opened. The waterwheel 340 would turn in the same counterclockwise direction with water flow in either direction. It is an objective of the present invention that no hatches or moveable trap doors be needed if a pair of concentric wings are used in a bi-directional tidal or ocean wave turbine.

FIG. 4 shows a convention for X, Y and Z axes relative to water flow, for example, from left to right water flow 410 (or up and down as in wave motion). The X axis is in-line with water flow 410 or air flow (wind). The Y axis horizontally crosses the flow of wind or water. A waterwheel shaft may be in the Y-axis. A vertical axis wind turbine may be in the Z-axis. The Z axis, for example, indicates a vertical direction, to transmit the harnessed energy vertically from right to left or left to right flow upward to a platform on which rests a controlling and generating module. The Z-axis is in-line with up and down ocean wave movement and may be used with concentric flat or rounded wings similar to those of an airplane or (triangular shaped with curved leading edges) concentric wings as will be suggested herein. A first embodiment of a concentric wing turbine (CWT) invention is for harnessing uni-directional river energy. Since the river energy is powerful and the flow of a river is in one direction, harnessing modules of uni-directional river turbines have to be strong and may harness and develop high torque and high energy because water has much greater mass than air. Air has lower density than water and will impact example wings with fixed flaps shown in FIG. 4D2 and angle of attack 830 shown in FIG. 8B.

FIG. 4A is a sketch of a helicopter 400 having a pair of opposing concentric wings 410A and 410B which are opposite one another. Notice that the support for each concentric wing is provided by a shaft extending the length of each wing at its center (a concentric wing). A motor/engine, not shown, applies torque to the hub and shaft 450 in one direction (clockwise) to rotate the propeller blades 410A and 410B to provide lift to the helicopter 400. It is hypothesized that the wings be concentric meaning that the leading edge of each concentric wing is concentric with the opposing shafts leaving each side of the hub and shaft 450. The rotating wings apply lift to lift the helicopter 400 off the ground and, when their rotational speed is reduced, for landing. If the helicopter is tilted forward and the tail lifted slightly, the helicopter 400 may move forward. It is also hypothesized that rotating helicopter wings of the concentric wing type may be similar to the opposing wings of a wind or river turbine harnessing module of concentric wings.

FIGS. 4B1 and 4B2 discuss the similarly facing symmetric wings of an airplane 480; (airplane wings are symmetrical relative to the body and create upward/downward lift, for example, using flaps (not shown). Concentric wings of a wind or river turbine need a shaft at the center of each wing to hold the two wings to the hub/shaft 130, 215 in opposition to one another and to create rotational lift, turning the shaft to turn the turbine. FIG. 4B1 shows a wing 485 in a downward direction 485A. When flaps (not shown) are turned downward or the wing is turned downward, the plane will begin to lose altitude. Drag is a force caused by, for example, flaps which slow a plane down or cause the plane to move downward. With wing 485B, the key is the angle of attack on wing 485B at the leading edge of the wing as it meets the air. The leading edge is somewhat circular or concentric (the center of the wing is located closer to the leading edge) which causes the force of Lift 491 to lift the plane because of the angle of attack of the wing on the air flow. In an exaggerated angle of attack as per wing 485C, the lift force 491 is even greater than with wing 485B until the airplane reaches a position of “stalling” and falling.

FIG. 4B2 shows with greater particularity the wing 485B and the steps of creating an upward force on a plane, namely, lift 491. In one step, the air splits at the front of the wing (the concentric edge). As the air passes over the wing, air pressure reduces at the top surface of the wing. The air follows the curvature of the top surface of the wing. On the other hand, at the third step, the air pressure is increased underneath the wing as a reaction to the angle of attack. At the trailing edge of wing 485B and step four, wind having passed over the upper surface and lower surface accelerates downward creating a downward force on the air leaving the trailing edge (creating an upward force on the plane or lift. These principles may be applied to concentric turbine wings as will be described herein.

FIGS. 4C1 and 4C2 are drawn to show designs of a concentric turbine wing where the wing of FIG. 4C1 has less curvature than the wing of FIG. 4C2. Wing 485 is less curved than wing 485B and produces little lift and drag. The wing 485B of FIG. 4C2 is a concentric wing with longer and a more curved trailing edge to obtain greater lift and drag. Greater lift and drag are desirable in opposite/concentric wings of a waterwheel or wind propeller. The degree of curvature is related to the density of air versus water and the required speed and torque for maximum rotation of the hub/shaft to which it is attached. Whether water flowing over the wing or wind flowing over the wing, the same principles of curvature (density of the medium, required speed and torque) applies.

FIG. 4C3 is intended to show definitions of terms used in describing a typical airplane wing profile view. The trailing edge 471 may typically be a sharp edge and is opposite a leading edge 474 which is curved. The radius of curvature is given by leading edge radius 476. A location of maximum wing thickness 477 is measured from the leading edge 474 as the radius from the maximum camber 461. Maximum camber location 475 (camber is arching at top and bottom wing surfaces) is related to the lengthwise thickness and is shown as maximum camber 461. A mean camber line 472 is denoted by the camber location along the wing width according to the arching of top and bottom wing surfaces. A chord line 462 runs horizontally straight from the leading edge 474 to the trailing edge 471. When straightened, this chord line is simply called a distance cord 473. Upper wing surface 465 is shown for the wing above lower wing surface 466. A plane wing is fixed to the plane at a leading angle of attack to the air. Flaps (not shown) are used to upper and lower the trailing edge 471 when taking off and landing.

FIGS. 4D1 and 4D2 show a front view and a side cut view section A-A respectively of an opposing, unidirectional turbine pair of concentric wings with one of the wings shown inside cut view FIG. 4D2. Terms from FIG. 4C3 are applied to FIGS. 4D1 and 4D2 as follows. Air or water flow toward the leading edge 474 (fixed flap 464 at the trailing edge) causes a counterclockwise rotation of shaft 465. Shaft 465 is typically round while hub 450 may be round, oval, square or rectangular as will be seen in subsequent drawings. Leading edge 474 is seen in section A-A from FIG. 4D1 as leading edge 474 of FIG. 4D2. An un-numbered opposing wing to wing 474 with fixed flap 464 is shown at the left of FIG. 4D1. A concentric wing turbine may have a curved upper surface 465 and a comparatively straight lower surface 463 but for a fixed flap 464 for creating a drag force per FIG. 4D2. A chord line 462 is shown running through the wing of a concentric wing side cut view in FIG. 4D2. In this example, water (or air) flows over a leading edge 474 and causes a counterclockwise rotation of the opposing concentric wings in front view FIG. 4D1. The water or wind flow in FIG. 4D2 is from bottom to top of FIG. 4D1 over the leading edge 474 to cause the wing to turn counterclockwise. “N” is defined as the number of pairs of concentric wings of a wind or river turbine. In this case, the turbine water flow is in one direction.

FIG. 5A, FIG. 5B and FIG. 5C pictorially show the X-axis, Y-axis and Z-axis 410 of FIG. 4. FIG. 5A is a photograph of an example of the X-axis as used herein. A propeller is shown receiving air flow in line with the propeller so that the depicted propeller feels the full flow of wind on its three propeller blades. FIG. 5B is a picture of a paddle wheel used at a site of a mill for horizontally receiving a flow of water diverted from a river or creek. As the water flows under the paddle wheel, the paddle wheel will turn as the water is captured by each vertical side of each paddle of perhaps one hundred paddles of the paddle wheel. This water flow is an example of horizontally crossing water flow or Y-axis water flow. Lastly, FIG. 5C is an example of vertically crossing wind flow or the Z-axis. FIG. 5C comprises six cupped, round surfaces vertically facing the wind. Any wind flow causes the six vertically mounted surfaces to turn about a shaft no matter what direction the wind if flowing any direction because of the cupped shape of the buckets.

FIGS. 6A and 6B are respective front and side views of multiple concentric blade/wing pairs (in this case, four blade pairs; N=4) mounted around a hub 450, the hub 450 (in this example, circular) surrounding a shaft 455 which, when it turns, harnesses energy from wind or river flow. The leading edges are lightly shaded. All blade/wings are in the same plane orthogonal to the direction of the shaft 455. Seen in side view FIG. 6B, the central pair of opposing blade/wings surrounds shaft 455 and N=1. N=2 is at 45° and when N=3, the blades/wings are orthogonal or at 90°. When N=4, the blades are at 135° and −45° showing the sharp, darker colored trailing edge. By “on a plane” is intended in a vertical plane (for receiving air or water from right or left) or in the same plane. In the next FIGS. 7A and 7B, there may be multiple planes.

FIGS. 7A and 7B shows four opposing pairs of concentric wings in three different planes in side view FIG. 7B mounted to hub 450 surrounding shaft 455, i.e. opposing blades on multiple horizontal planes. Hub 450 is elongated and comprises three hubs (cylinders) in FIG. 7B such that each wing pair turns around shaft 455 and the hubs 450 in FIG. 7B may be other than circular as seen in front view FIG. 7A.

FIG. 8A is a photograph of a bi-directional Osprey helicopter 800 having propellers 810 mounted on a tilt-controlled motor/engine 830 and oppositely turning propeller 820 mounted on a tilt-controlled motor/engine 840. There is a typical concentric airplane wing seen connecting the two engine-driven propellers 810, 820. The airplane/helicopter 800 may go vertically up and down and forward depending on engine speed and propeller tilt and direction.

FIGS. 8A1 through 8A6 show various flying alternatives of the Osprey airplane/helicopter 800 (Bell Boeing V-22 Osprey) of FIG. 8A. In side view FIG. 8A, front view FIG. 8A2 and top view FIG. 8A3, it is seen that the propellers are facing forward for flying like an airplane flies and so the airplane/helicopter flies in a similar manner to a propeller-driven airplane in FIG. 8A1 and takes off and lands like a helicopter per FIGS. 8A4, 8A5 and 8A6 (side views). FIGS. 8A2 (flying forward) and 8A5 (landing or taking off) are front views. The Osprey of FIG. 8A2 with its large propellers move the Osprey forward out of the page toward the viewer. FIG. 8A5 shows lift-off or landing as a helicopter. FIGS. 8A3 and 8A6 are top views of the Osprey. In FIG. 8A3, the Osprey flies from left to right. In FIG. 8A6 the Osprey is landing or taking off.

In summary, FIG. 8A4 is a side view of the Osprey 800 in a vertical take-off mode or landing mode (moving upwards or downwards); FIG. 8A5 is a front view of the Osprey of FIG. 8A4. FIG. 8A6 is a top view of the Osprey of FIG. 8A4. FIGS. 8A1 through 8A3 are side view, front view and top views of an airplane mode of operation. FIGS. 8A4 through 8A6 are views of a helicopter mode of operation. Concentric wings for flying are seen best in perspective view FIG. 8A.

FIG. 8B is a cross-sectional view of an aerofoil 840 for a bi-directional tidal wing turbine where the angle of attack a 830 on the depicted wing is the angle between the free air (or water) stream and the aerofoil 840 having chord 473. A resultant force 493 between lift 491 and drag 492 for aerofoil 840 given angle of attack 830 shows that the lift 491 is less than the drag 492 but the resultant 493 is a positive force upward and to the right causing the aerofoil concentric wing to turn upon impact with the water (or air) hitting the leading edge 474. In the case of a concentric wing pair rotatable about a shaft and receiving an air (or water) stream at its concentric wing sides, the resultant will turn the concentric wing in the direction of air (or water) flow; (picture a fan blade freely turning due to air hitting the fan blades when the fan motor is turned off). Aerofoil 840 may have application in a bi-directional tidal turbine comprising opposing aerofoils surrounding a hub. For example, if there is a wind blowing on a fan that has had its motor turned off, the fan blades will turn when the wind hits the leading edges of the fan blades.

FIG. 8C shows the phenomenon of upwash and downwash on a bi-directional tidal turbine concentric wing. From FIG. 8B, we note that the forces acting on a typical aerofoil 840 section of an axial flow fan blade are lift 491 caused by the free air (or water) stream hitting the blade at an angle of attack a 830 and drag 492 with a resultant force 493 shown.

As can be seen from FIG. 8C, a complication may occur due to the effect of upwash/downwash caused by the angle of attack on an upturned wing at the upward leading edge 474 of the concentric wing (blade). The air/water flowing over the concentric wing upper surface tends to hug the upper wing surface rather than proceeding upward. Thus, the upwash tends to create a negative lift and thus it needs to be compensated by pushing more air down at the lower trailing edge 474. Also evident from FIG. 8C is the fact that the top wing surface does much more to move the air than the bottom surface. Hence, the top surface of the wing is the more critical surface. Downwash (air following the top surface of the wing) at the trailing edge 471 can be accentuated by downward flaps that create drag and cause, for example, top and bottom surface air flow to wash downward.

FIGS. 8D1 and 8D2 show front and top views respectively of a bi-directional wing turbine that uses an actuated rack and pinion (seen in FIG. 8D2) to set the left and right concentric wings 810A and 820B at an in line or horizontal position orthogonal to the shaft 855 and hub 850. Section A-A shows the left concentric wing 810A and section B-B shows the right concentric wing 820B. In this figure, the left wing and the right wing are not distinguishable from one another having similar leading and trailing edges and concentric centers. Per FIG. 8D2, the top view, section C-C shows that the rack and pinion for the left wing or right wing to be in line or horizontal are centered (stationery at center). Also, as per FIG. 8D2, the top view, section D-D shows that the rack and pinion for the right wing to be in line or horizontal are centered (stationary at center).

FIGS. 8D3 and 8D4 show front and side cut views respectively when the left concentric wing 810A and right concentric wing 820B are facing 45° toward the upper left and 45° toward the upper right respectively (in side view sections A-A and B-B). It may be clearly seen that the left and right wings may be rack and pinion operated such that when the rack and pinion rotate clockwise to a down position (section C-C) and the right rack gear is rotated counterclockwise to the down position, the wing turbine may be bi-directional without the need for a hatch and paddle or van or trap doors as per FIGS. 2A, 2B, 3A and 3B when water or air flow in either direction of flow. In particular, FIGS. 8D5 and 8D6 show wind change from left to right to right to left respectively with reference to side views of wings 810B and 820B.

FIGS. 8D5 and 8D6 show air or water flows from the left and right respectively creating lift on either of wings 810B and 820B (same or different wings). The wings 810B and 820B are rack and pinion actuated to be either pointing 45° toward the upper left to create lift when air/water flow is from the left or 45° toward the upper right to create lift when air/water flow is from the right. Wings 810B and 820B may be mounted opposite one another and connected to shafts to a hub not shown for receiving water flow from the left or the right and together turn in the same direction of rotation regardless of air/waterflow direction.

FIGS. 9A and 9B show another position of bi-directional concentric wings of a turbine, namely, the rack and pinion gears have moved the left wing to be pointing up while the right wing is pointing down. Note that per FIG. 9B, the left wing is pointing up perpendicular to the turbine shaft while the right wing is pointing down as actuated by the rack and pinion gears (not shown). The right wing 920B is coming out of the page from the hub opposite wing 910B which extends into the page.

FIG. 9A is repeated in the next sheet of drawings comprising FIGS. 9A through 9F missing any FIG. 9B. FIGS. 9C through 9F show different angles of attack, directions of air/water flow and directions of left and right opposite wings of lift force. As already shown, FIG. 9A shows a front view of a bi-directional concentric wing turbine harnessing module with a counterclockwise rotation about turbine shaft 955 and hub 950. FIG. 9A shows left wing 910B pointing up and right wing 920B pointing down. Now, assuming that air/water flows from left to right, FIG. 9C shows a right-side view of left wing 910B where the angle of attack 930A is negative and wing 910B is moved clockwise from pointing up to pointing down while the direction of air/water flow is from left to right. The lift force 942 is downward. Stop is indicated as 940 for the given angle of attack. (FIG. 9E is also a right-side view of the left wing but the direction of air/water flow is from right to left and is discussed later). FIG. 9D is another view of the direction of air flow from left to right with the angle of attack 930C pointed at a right wing 920B moving counterclockwise from vertical to an upward lift position so that the resulting lift 944 is upward. Stop position 940 is shown for the given angle of attack 930C. Now referring to FIG. 9E and FIG. 9F the respective angles of attack and direction of air/water flow is from right to left. In FIG. 9E, the concentric wing 920B moves from a vertical position counterclockwise to a position for downward or a negative lift force. The right-side view of the left wing 930B shows downward lift 942 with the air/water flow from right to left. Lastly, FIG. 9F shows a right side view of right wing 920B. Right wing 920B is moved clockwise from a vertical position to a position having an angle of attack 930D. The resultant lift force is positive or upwards. Stop position 940 is shown at the top left surface of wing 920B.

FIGS. 10A through 10G and FIGS. 10A1 through 10N1 show bi-directional concentric “boomerang” wings. A triangular wing is introduced in profile having concentric centers 1060 in a brief description of FIGS. 10A-10G. FIGS. 11A and 11B show two sets of counter-rotating fixed wing turbines. Wave motion is either from one side or the other per FIGS. 11A and 11B. Sprags (one-way clutch bearings (OWCB)) are shown to cause proper engagement of the boomerang wing pairs depending on air/water flow direction. (An electromechanical system may also be used).

FIG. 10A shows a front view of a left triangular wing 1010B and right triangular wing 1020B mounted opposite one another around a turbine shaft 1055 and hub 1050 which are orthogonal to a concentric wing support shaft 1060. When seen in front view they are shown as concentric wings with a curved leading edge and when seen in section, the triangular concentric wings may have curved sides as well as curved leading edges and are called boomerang wings. Clockwise rotation of the left wing with section A-A is shown in FIGS. 10B, 10C and 10D with different air/water flow directions (no flow, flow from left and flow from right respectively).

FIG. 10B shows a position of the left triangular wing section A-A where the is no air or water flow direction and the left wing is facing upward.

FIG. 10C shows the left wing of FIG. 10A receiving air/water flow from the left and the left triangular wing tilting rotationally counterclockwise according to the angle of attack not shown and the flow is strong enough that the right side of the left triangular wing is horizontally stopped by stop 1040.

FIG. 10D shows the left wing of FIG. 10A receiving air/water flow from the right and the triangular wing tilting rotationally clockwise according to the angle of attack (not shown) and the flow is strong enough that the right side of the left triangular wing is horizontally stopped by stop 1040.

FIGS. 10E through 10G show section B-B of the right triangular wing where FIG. 10E shows the right wing facing downward with no air or water flow. FIG. 10F shows air or water flow from the left and the triangular wing still facing downward but, receiving the air or water flow from the left being tilted to face down but receive the wind or water flow at an angle of attack not shown forcing the left side of the right wing up slightly while the right side is in line with the air or water flow.

FIGS. 10A1 through 10N1 show further views of concentric “boomerang” wing turbines, particularly the harnessing module component. For example, FIG. 10A1 shows a front view when there is no water or air flow of boomerang wings. FIG. 10B1 is the related side view of the boomerang wings surrounding shaft 1060 with no flow. FIGS. 10C1 through 10N1 show further views with different flows, with left or right wing up or down and FIGS. 10M1 and 10N1 show the same clockwise rotation whether the flow direction is up or down. Samples 7A and 7B of FIGS. 10C1 and 10E1 have been built and tested with each direction of flow shown.

FIGS. 11A and 11B show two sets of counter-rotating fixed triangular wing turbines having one-way clutch bearings (OWCB's or sprags) for turning the turbine in the same direction whether air/water flows from the right to left (FIG. 11A) or the left to right (FIG. 11B). In FIG. 11A, the left turbine rotates clockwise because the left Sprag is engaged and the right turbine rotates counterclockwise. In FIG. 11B, the right turbine rotates clockwise when the right Sprag is engaged and the left turbine rotates counterclockwise.

The figure descriptions above are intended to be brief descriptions of the drawings.

Following the brief description of the drawings is a more detailed description of the drawings which are not intended to be limited by the above brief description of the drawings.

DETAILED DESCRIPTION

Similar references characters will be used in the following detailed description of concentric wing embodiments where the first number of a reference numeral such as 1XX may indicate the Figure number where the element first appears and the XX may indicate a similar element such as a protector bar 190 seen in FIG. 1B where 1 is the figure number and ninety is the component number.

Referring to FIGS. 1A and 1B, FIG. 1A is a front view of a river turbine mounted on a platform 150 that may be tied to a river bottom or to river banks. FIGS. 1A and 1B each comprise assemblies of a platform 150 intended to float on a water surface and may comprise a concentric wing turbine with at least one pair of concentric wings per FIGS. 8D1 and 8D2. A problem with water flow turbines in cold climates is that, for example, a river may freeze in winter months, for example, if located in Canada, and the use of a river turbine in such a cold climate may be limited. Concentric wings 120C and 120G, for example, form an opposing pair of concentric wings 195 surrounding a hub and a drive or turbine shaft 130 where the hub may be circular, oval, square or rectangular. Its harnessing module is identified by blades 120A through 120H tied/attached to a turbine shaft 130. The harnessing module is under water and captures water flow energy from concentric wings 120A through 120H seen in FIG. 1A while a concentric wing 195 is seen in side view FIG. 1B. Per FIG. 1B the turbine shaft 130 may be a driving component of a chain box 188 which is vertically connected to a set of chain and sprockets 189 for driving a speed converter 145 (for example, a spur gear assembly or control module) which has three variables one variable being an input from the harnessing module and rotating concentric wings, an output to the generator 155 an a control motor 135 for connection to the speed converter 145 being a control variable. FIG. 1B is a side view of the turbine of FIG. 1A proposing that a concentric wing 195 be used as a blade 120A through 120H. In FIGS. 1A and 1B, river turbines may be typically mounted on floating platforms 150 having a support plate 192 for hardware components except the chain box 188. As discussed herein the turbine blades may look like airplane wings but are structured and designed for use as harnessing module concentric wings. It is an object of the present invention to study airplane wings such as concentric wings for the purpose of harnessing greater energy amounts than is known from using paddles, buckets, blades or propeller blades known in the art.

In FIGS. 2A and 2B there is shown an example of a harnessing module mounted under floating platform 210. A hatch 220 may be attached to/surrounded by a paddle or vane 240 so that the hatch 220 may move to the position shown in FIG. 2A with water flow from the right to left through one side of the harnessing module because of the water flow controlling the location of the paddle or vane 240. The hatch 220 may move (swing around the waterwheel 230 with a change in water flow direction from right to left to left to right, FIG. 2A to FIG. 2B) to the opposite side to the position shown in FIG. 2B when the water flow is from left to right when the paddle of vane 240 catches the water flow from left to right.

Referring to FIG. 3A and FIG. 3B, there is shown a front view and a side view respectively of a waterwheel having protector bars 310, 320 for protecting the waterwheel from floating debris (and also stopping debris from flowing between the protector bars 310/320). The protector bars can also prevent water flow from reaching the waterwheel channeling the water away from the top or bottom half of the waterwheel 340. Moveable trap doors 330 on the other hand operate with different directions of water flow to permit water to be released by the waterwheel when the direction of water flow is from right to left as shown in FIG. 3B. If water flow were from left to right, the top left moveable trap door would stop water from going to the top of the waterwheel while the bottom left protector bar would allow water to reach the bottom half of the waterwheel 340. Thus, the waterwheel of FIGS. 3A and 3B may also be used for bi-directional water flow by action of the moveable trap doors 330. The hub and turbine shaft 350 are shown in FIG. 3B. Waterwheel 340 rotation can be bi-directional and be controlled, for example, with the protector bars 310/320 stationary and the moveable trap doors 330 moved to an open or closed position depending on the direction of water flow—right to left water flow being shown in FIG. 3B with a hatch or trap doors 330. Referring now to FIG. 3B, there is shown a side view with water flowing from right to left. Note that the water flow closes the bottom right trap door 330 (at the right) and opens the top left trap door 330 (at the left) when water flows from right to left. So, the top half of the waterwheel is used in FIG. 3B with water flowing from right to left through the protector bars 310, 320. If water flowed in the opposite left to right direction, the right bottom trap door 330 (at the bottom) would be opened and the waterwheel would turn in the same counterclockwise direction. It is an objective of the present invention that no hatches or moveable trap doors be needed if a pair of concentric wings are used in a bi-directional tidal or ocean wave turbine.

FIG. 4 shows a convention for X, Y and Z axes relative to water flow, for example, from left to right (or up and down as in wave motion). The X axis is in-line with water flow or air flow (wind) direction 410. Another way of saying in-line is that the X-axis if a waterwheel shaft would capture the energy flow of water from left to right 410 (or the reverse direction, not shown) would cause a waterwheel to turn if mounted on the Y-axis. The Y-axis horizontally crosses the flow of wind or water. A waterwheel shaft may be in the Y-axis. A vertical axis wind turbine may be in the Z-axis. The Z axis, for example, indicates a vertical direction, to transmit the harnessed energy vertically from right to left or left to right flow upward to a platform on which rests a controlling and generating module. The Z-axis is in-line with up and down ocean wave movement and may be used with concentric or triangular shaped wings as will be suggested herein. A first embodiment of a concentric wing turbine (CWT) invention is for harnessing uni-directional river energy. Since the river energy is powerful and the flow of a river is in one direction, harnessing modules of uni-directional river turbines have to be strong, produce greater torque and may harness and develop high torque and high energy because water has much greater mass or density than air.

FIG. 4A is a sketch of a helicopter 400 having a pair of opposing concentric wings 410A and 410B which are opposite one another. There is a wing shaft, un-numbered, that passes through the concentric wing at its center and can rotate the wing slightly to increase or decrease its angle of attack (see FIG. 8B, angle α). A motor/engine, not shown, applies torque to the hub and shaft 450 in one direction (clockwise) to rotate the propeller blades 410A and 410B resulting in lift. It is hypothesized that the wings be concentric meaning that the leading edge of each concentric wing is concentric with the opposing wing shafts leaving each side of the hub and shaft 450. The rotating wings apply lift to lift the helicopter 400 to lift the helicopter off the ground and for landing. If the helicopter is tilted forward and the tail lifted slightly, the helicopter 400 may move forward. It is also hypothesized that rotating helicopter wings of the concentric wing type may be similar to the opposing wings of a turbine of concentric wings. The un-labeled rotor propeller at the end of the helicopter is for stability and can control direction of helicopter 400 motion.

FIGS. 4B1 and 4B2 discuss the similarly facing symmetric wings of an airplane 480 where there may be concentric wings 485 mounted approximately as show in side view for forward movement by propeller action; (airplane wings are symmetrical relative to the body and create upward/downward lift). Concentric wings may need a shaft to hold the two wings in opposition and to create rotational lift in a helicopter but not in an airplane which have wing flaps (not shown) to change the angle of attack. FIG. 4B1 shows a wing 485 in a downward direction 485A but a flap is not shown for causing the downward direction of forward movement. When flaps (not shown) are turned downward or the wing is turned downward (so the flaps point upward), the plane 480 will begin to lose altitude. Drag is a force caused by, for example, flaps which slow a plane down or cause the plane to move upward or downward. With wing 485B, the key is the angle of attack on wing 485B at the leading edge of the wing which is somewhat circular or concentric (as will be discussed further herein) which causes the force of Lift 491 to lift the plane 480 as it is propelled forward. In an exaggerated angle of attack as per wing 485C, the lift force 491 is even greater than with wing 485B until the airplane reaches a position of “stalling” (a phenomenon where a pilot can lose control of their airplane and the airplane crash).

FIG. 4B2 shows with greater particularity the wing 485B and the steps of creating an upward force on a plane, namely, lift 491. In one step, the air splits at the front of the wing (the concentric wing edge). As the air passes over the wing, air pressure reduces at the top surface of the wing. The air follows the curvature of the top surface of the wing. On the other hand, at the third step, the air pressure is increased underneath the wing as a reaction to the proper angle of attack for lift. At the trailing edge and step four, wind having passed over the upper and lower surfaces of the wing accelerates downward creating a downward force on the air leaving the trailing edge. Generally, the wing 485B lifts the plane because the amount of lift lifts the plane to a higher altitude (without the plane stalling). These principles may be applied to concentric turbine wings as will be described herein.

FIGS. 4C1 and 4C2 are drawn to show a design of a concentric turbine wing where the wing of FIG. 4C1 has less curvature than the wing of FIG. 4C2. (There is an accentuated flap, not shown, in FIG. 4C2 at the trailing wing edge.) The wing 485B of FIG. 4C2 is a concentric wing with longer and a more curved trailing edge to obtain greater lift and drag than the flatter wing of FIG. 4C1. Greater lift and drag are desirable in opposite/concentric wings of a waterwheel or wind propeller. Whether water flow or wind flow, the same principle applies.

FIG. 4C3 is intended to show definitions of terms used in describing a typical concentric airplane wing profile view. The trailing edge 471 may typically be a sharp edge and is opposite a curved leading edge 474 which is curved to a degree according to its radius of curvature given by leading edge radius 476. A location of maximum wing thickness 477 from the leading edge 474 is measured from the leading edge 474 to a location of maximum thickness. Maximum camber location 475 (camber is arching at top and bottom wing surfaces) is related to the lengthwise curvature at upper and lower surfaces and is shown as maximum camber 461. A mean camber line 472 is denoted by the camber location along the curved wing width according to the arching or curving of top and bottom wing surfaces. A chord line 462 runs horizontally straight from the leading edge 474 to the trailing edge 471. When straightened, this chord line is simply called a distance cord 473 having a measurable distance. Upper wing surface 465 is shown for the wing directly above lower wing surface 466.

FIGS. 4D1 and 4D2 show a front view and a side cut view section A-A respectively of an opposing, unidirectional pair of concentric wings of turbines for air or water with one of the wings shown in side cut view FIG. 4D2 forming side cut view section A-A. Terms from FIG. 4C3 are applied to FIGS. 4D1 and 4D2 as follows. Turbine shaft 465 is typically round while hub 450 may be round, oval, square or rectangular (round shown) as will be seen in subsequent drawings. Wing shafts (unnumbered) support the concentric wings at their centers. Leading edge 474 and fixed flap 464 of the right wing are seen in section A-A from FIG. 4D1 as leading edge 474 through fixed flap 464 of FIG. 4D2. An un-numbered opposing wing to wing 474 with fixed flap 464 is shown at the left of FIG. 4D1. A concentric wing turbine may have a curved upper surface 465 and a comparatively straight lower surface 463 but for a fixed flap 464 for creating a drag force per FIG. 4D2. A chord line 462 is shown running through the wing of a concentric wing side cut view in FIG. 4D2. In this example, water (or air) flows over a leading edge 474 and causes a counterclockwise rotation of the opposing concentric wings in front view FIG. 4D1. The water or wind flow in FIG. 4D2 is from bottom to top of FIG. 4D1 over the leading edge 474 to cause the wings to turn counterclockwise. “N” is defined as the number of pairs of concentric wings of a wind or river turbine. In this case, the turbine water flow is in one direction and N equals one pair of wings.

FIG. 5A, FIG. 5B and FIG. 5C pictorially show the X-axis, Y-axis and Z-axis 410 of FIG. 4. FIG. 5A is a photograph of an example of the X-axis as used herein. A propeller is shown receiving air flow in line with the propeller so that the depicted propeller feels the full flow of wind on its three propeller blades. FIG. 5B is a picture of a paddle wheel used at a site of a mill for horizontally receiving a flow of water diverted from a river or creek according to the Y-axis or a horizontal crossing of the waterwheel. As the water flows under the paddle wheel, the paddle wheel will turn as the water is captured by each vertical side of each paddle of perhaps one hundred paddles of the paddle wheel as the wheel turns. This water flow is an example of horizontally crossing water flow or Y-axis water flow. Lastly, FIG. 5C is an example of vertically crossing wind flow or the Z-axis. FIG. 5C comprises six cupped, round surfaces vertically facing the wind. Any wind flow in any direction causes the six vertically mounted surfaces to turn about a shaft no matter what direction the wind is flowing from.

FIGS. 6A and 6B are respective front and side views of multiple blade/wing pairs (in this case, four blade pairs; N=4) mounted around a hub 450, the hub 450 (in this example, circular) surrounding a shaft 455 which, when it turns, harnesses energy from wind or river flow. The wing shafts are shown but not numbered in this drawing but the shorter, lighter shaded hatching identifies the leading edges of each wing. All blade/wings are in the same plane orthogonal to the direction of the shaft 455 and located at an undisclosed angle of attack. Seen in side view FIG. 6B, the central pair of opposing blade/wings surrounds shaft 455 and N=1. N=2 is at 45° and when N=3, the blades/wings are orthogonal or at 90°. When N=4, the blades are at 135° and −45° showing the sharp, darker shaded trailing edge. By “multiple blades on a plane” is intended in a vertical plane (for receiving air or water from right or left) or in the same plane. In the next FIGS. 7A and 7B, there may be multiple planes.

FIGS. 7A and 7B shows four opposing pairs of concentric wings in four different planes surrounding turbine shaft 455, i.e. opposing blades on multiple horizontal planes. Hub 450 is elongated and comprises three hubs (cylinders) in FIG. 7B such that each wing pair turns around shaft 455 and the hubs 450 in FIG. 7B may be other than circular as seen in front view FIG. 7A. When N equals 2 or 4, the wings may be in the same plane.

FIG. 8A is a photograph of a bi-directional Osprey helicopter 800 having propellers 810 mounted on a tilt-controlled motor/engine 830 and oppositely turning propeller 820 mounted on a tilt-controlled motor/engine 840. There is a typical concentric airplane wing seen connecting the two engine-driven propellers 810, 820 for forward motion (not numbered). The airplane/helicopter 800 may go vertically up and down and forwards depending on engine speed and propeller tilt and direction. The concentric wing is located above the plane and carries both propeller engines which rotate per FIG. 8A1-8A6

FIGS. 8A1 through 8A6 show various flying alternatives of the Osprey airplane/helicopter 800 (Bell Boeing V-22 Osprey) of FIG. 8A. In side view FIG. 8A1, front view FIG. 8A2 and top view FIG. 8A3, it is seen that the propellers are facing forward for flying as a propeller-driven airplane flies forward and so the airplane/helicopter flies in a similar manner to a propeller-driven airplane in FIG. 8A1 and takes off and lands like a helicopter per FIGS. 8A4, 8A5 and 8A6 (side view, front view and top view). FIGS. 8A2 (flying forward) and 8A5 (landing or taking off) are front views. The Osprey of FIG. 8A2 with its large propellers move the Osprey forward out of the page toward the viewer. FIGS. 8A4, 8A5 show lift-off or landing as a helicopter. FIGS. 8A3 and 8A6 are top views of the Osprey flying from left to right in FIG. 8A3 or landing or taking off in FIG. 8A6.

In summary, FIG. 8A4 is a side view of the Osprey 800 in a vertical take-off mode or landing mode (moving upwards or downwards); FIG. 8A5 is a front view of the Osprey of FIG. 8A4. FIG. 8A6 is a top view of the Osprey of FIG. 8A4 or 8A5. FIGS. 8A1 through 8A3 are side view, front view and top views of an airplane mode of operation. FIGS. 8A4 through 8A6 are views of a helicopter mode of operation. Concentric wings for flying are seen best in perspective view FIG. 8A.

FIG. 8B is a cross-sectional view of an aerofoil 840 for a bi-directional tidal wing turbine where the angle of attack a 830 on the depicted wing is the angle between the free air stream and the aerofoil 840 having chord 473. A resultant force 493 between lift 491 and drag 492 for aerofoil 840 given angle of attack 830 shows that the lift 491 is less than the drag 492 but the resultant 493 is a positive force upward causing the aerofoil concentric wing to turn upon impact with the water (or air) hitting the leading edge 474. Angle of attack 830 may vary with a position of a wing shaft (not shown). In the case of a concentric wing pair rotatable about a turbine shaft and receiving an air stream at its concentric wing sides, the resultant will turn the concentric wing in the direction of air flow; (picture a fan blade freely turning due to air hitting the fan blades when the fan motor is turned off). Aerofoil 840 may have application in a bi-directional tidal turbine comprising opposing aerofoils surrounding a hub. For example, if there is a wind blowing on a fan that has had its motor turned off, the fan blades will turn when the wind hits the leading edges of the fan blades.

FIG. 8C shows the phenomenon of upwash and downwash on a bi-directional tidal turbine concentric wing. From FIG. 8B, we note that the forces acting on a typical aerofoil 840 section of an axial flow fan blade are lift 491 caused by the free air stream hitting the blade at an angle of attack a 830 and drag 492 with a resultant force 493 shown.

As can be seen from FIG. 8C, a complication may occur due to the effect of upwash/downwash caused by the angle of attack on an upturned wing at the upward leading edge 474 of the concentric wing (blade). The air/water flowing over the concentric wing upper surface tends to hug the upper wing surface rather than proceeding upward. Thus, the upwash tends to create a negative lift and thus it needs to be compensated by pushing more air down at the lower leading edge 474. Also evident from FIG. 8C is the fact that the top wing surface does much more to move the air than the bottom surface. Hence, the top surface of the wing is the more critical surface. Downwash (air following the top surface of the wing) at the trailing edge 471 can be accentuated by downward flaps that create drag and cause, for example, top and bottom surface air flow to wash downward.

FIGS. 8D1 and 8D2 show front and top views respectively of a bi-directional wing turbine that uses an actuated rack 865 (rack gear) and pinion 870 (circular gear) (both rack and pinion seen in FIG. 8D2) to set the left and right concentric wings 810A and 820B at an in line or horizontal position orthogonal to the turbine shaft 855 and hub 850. Notice that the circular gear or pinion 870 is in the middle of the rack gear 865 for placing the wing 810A, 810B in a horizontal position (FIG. 8D1). The pinion 870 may be moved on rack 865 by a motor not shown. The angle of attack of the wings is 00. Section A-A shows the left concentric wing 810A and section B-B shows the right concentric wing 820B. In this figure, the left wing and the right wing are not distinguishable from one another having similar leading and trailing edges. Per FIG. 8D2, the top view, section C-C shows that the rack and pinion for the left wing or right wing to be in line or horizontal are centered (stationery at center). Also, as per FIG. 8D2, the top view, section D-D shows that the rack 865 and pinion 870 for the right wing to be in line or horizontal are centered (stationary at center).

FIGS. 8D3 and 8D4 show front and side cut views respectively when the left concentric wing 810A and right concentric wing 820B are facing 45° toward the upper left and 45° toward the upper right respectively (in sectional A-A and B-B views). Referring to FIG. 8D4, the pinion 870 has been rotated clockwise downward in sectional view C-C. For the left wing to have an angle of attack of 45° the pinion 870 has moved clockwise down the rack 865. On the other hand, the right wing has an angle of attack of −45° and the pinion 870 has been moved counterclockwise down the rack 865 in sectional view D-D. It may be clearly seen that the left and right wings may be rack 865 and pinion 870 operated. When the rack and pinion rotate clockwise to a down position (section C-C) and the right rack gear is rotated counterclockwise to the down position, the wing turbine may be bi-directional without the need for a hatch and paddle or a vane or trap doors as per FIGS. 2A, 2B, 3A and 3B when water or air flow is in either direction of flow. In particular, FIGS. 8D5 and 8D6 show wind change from left to right and from right to left respectively with reference to sectional views of wings 810B and 820B. Each wing shaft 860 turns each wing so that flow from either direction can cause lift or torque on the turbine shaft (not shown).

FIGS. 8D5 and 8D6 show air or water flows from the left creating lift and air or water flow from the right creating lift on wings 810B and 820B (same or different wings). The wings 810B and 820B are rack and pinion actuated to be either pointing 45° toward the upper left to create lift when air/water flow is from the left or 45° toward the upper right to create lift when air/water flow is from the right. Wings 810B and 820B may be mounted opposite one another and connected to a hub and shaft (not shown) for receiving water flow from the left or the right and together turn in the same direction of rotation regardless of air/water flow direction.

FIGS. 9A and 9B show front views and right side views respectively of bi-directional concentric wings for an air or water turbine. FIGS. 9A and 9B another position (wings straight up and down) of bi-directional concentric wings of a turbine, namely, the rack and pinion gears have moved the left wing to be pointing up while the right wing is pointing down. The turbine is rotating around the turbine shaft 955. Wing shaft 960 defines the curved leading edge of a concentric wing from the trailing edge (shown as more pointed for simplification). Note that per FIG. 9B, the left wing is pointing up perpendicular to the turbine shaft 955 while the right wing is pointing down as actuated by the rack and pinion gears (not shown). The right wing 920B is coming out of the page from the hub opposite wing 910B which extends into the page. (The hub is pictured as square or rectangular in FIG. 9A).

FIG. 9A is repeated in the next sheet of drawings, FIGS. 9A through 9F (missing FIG. 9B). FIG. 9A clearly shows counterclockwise rotation of the shaft 955 when direction of flow hits the leading edge per FIGS. 9C through 9F. FIGS. 9C through 9F are added to show different angles of attack, directions of air/water flow and directions of left and right opposite wings of lift force. As already shown, FIG. 9A shows a front view of a bi-directional concentric wing turbine harnessing module with a counterclockwise rotation about turbine shaft 955 and hub 950. FIG. 9A shows left wing 910B pointing up and right wing 920B pointing down. Now, assuming that air/water flows from left to right (flow direction arrow), FIG. 9C shows a right-side view of left wing 910B where the angle of attack 930A is negative and wing 910B is moved clockwise from pointing up to pointing to the side to a stop 940 while the direction of air/water flow is from left to right. The lift force 942 is downward. Stop is indicated as 940 for the given angle of attack (perhaps about 50°. (FIG. 9E is also a right-side view of the left wing but the direction of air/water flow is from right to left as with FIG. 9F. FIGS. 9E and 9F are discussed later with the opposite angle of attack). FIG. 9D is another view of the direction of air flow from left to right with the angle of attack 930C pointed at a right wing 920B moving counterclockwise from vertical to an upward lift position at stop 940 so that the resulting lift 944 is upward. Stop position 940 is shown for the given angle of attack 930C. Wing shaft 960 is also shown about which wing 920B rotates. Now referring to FIG. 9E and FIG. 9F, the respective angles of attack and direction of air/water flow is from right to left. In FIG. 9E, the concentric wing 920B moves from a vertical position counterclockwise to a position for downward or a negative lift force at stop 940. The right-side view of the left wing 930B shows downward lift 942 with the air/water flow from right to left at angle of attack 930B. Lastly, FIG. 9F shows a right side view of right wing 920B. Right wing 920B is moved clockwise from a vertical position to a position having an angle of attack 930D at stop 940. The resultant lift force upward 944 is positive or upwards. Stop position 940 is shown at the top left surface of wing 920B which rotates about wing shaft 960.

Now, a triangular (a developed “boomerang profile) wing is introduced in a brief description of FIGS. 10A-10G (first sheet of FIG. 10), FIGS. 10A1-10F1 (second sheet of FIG. 10), FIGS. 10A1, 10C1 and IOEI (third sheet of FIG. 10); FIGS. 10G1-10N1 (fourth sheet of FIG. 10) and 11A-11B (sprag or one way clutch bearing (OWCB) engagement depending on flow direction). FIGS. 11A and 11B show flow directions from left and right respectively. FIG. 1 IA show engagement of left one-way clutch bearing so the left turbine rotates clockwise and the right turbine rotates counterclockwise. When flow is from right to left as in FIG. 11B, the right sprag engages, the right turbine rotates clockwise and the left turbine rotates counterclockwise. A “developed profile” as used herein for the triangular or “boomerang” wing shapes shown in FIGS. 10A through 10G, FIGS. 10A1 through 10N1 and FIGS. 11A through 11B means that the developed profile is not a certain known concentric profile having a curved leading edge, but a profile that was experimentally developed for use with a turbine according to the invention of these Figures that may be shaped more like a boomerang than a triangle. A curved leading edge is preferred and curved wing (sides of the triangle) are preferred. Further experiments with different profile wings may result in the development of different shapes of profiles besides a triangular (or a boomerang) profile with a concentric, curved leading edge. Wave motion is either from one side or the other per FIGS. 11A and 11B. Sprags (one-way clutch bearings (OWCB)) are shown in these figures to cause proper engagement of the triangular (boomerang) turbine wings depending on air/water flow direction. (An electromechanical system may also be used).

FIG. 10A shows a front view of a left triangular (developed boomerang profile) wing 1010B and right triangular wing 1020B mounted opposite one another around a turbine shaft 1055 and hub 1050 and supported by a wing shaft 1060. Clockwise rotation with sections A-A and B-B is shown for left wing 1010B and right wing 1020B. In FIGS. 10B, O1C and 10D with different air/water flow directions (no flow, flow from left and flow from right respectively) are shown. The left wing 1010B, sectional view A-A is not moved with no flow; moved to the left in FIG. 10C with flow from the left to stop position 1040 and moved to the right with flow from the right to stop 1040 for example by rack and pinion (not shown).

In FIGS. 10E (Section B-B of right wing 1020B, no flow), 10F and 10G with different air/water flow directions (no flow, flow from left and flow from right respectively), the right wing 1020B is shown at section B-B. The right wing 1020B is not moved in FIG. 10E with no flow and no movement about shaft 1060; wing 1020B (section B-B) is moved to the left in FIG. 10F to stop 1040 with flow from the left around shaft 1060 and moved to the right in FIG. 10G with flow from the right to stop 1040 about shaft 1060.

FIGS. 10A1 through 10F1 show front and side views of concentric boomerang wing turbine harnessing module wing components with either no flow, flow from left to right or flow from right to left. The unnumbered horizontal shaft is not receiving any flow in FIG. 10A1. The boomerang wing profiles are in an at rest position. Similarly, in side view FIG. 10B1, one sees the slim height of each wing and not its full extension. On the other hand, in FIG. 10C with flow from the left, one sees movement of the wing profiles so that in FIG. 10D1, the lighter diagonally shaded wing is shown to the left and the darker diagonally shaded wing is to the right in side view when flow is from left to right. In FIGS. 10E1 and 10F1, the light shading and darker shading of the wings are vertical. The flow is from the right to the left per front view FIG. 10E1. In side view FIG. 10F1 side view, the lighter vertical shaded boomerang wing is seen to the left and the darker, vertically shaded wing is seen to the right.

A second sheet shows isolates FIG. 10A1 with light and dark shading from FIG. 10C1, front view with flow from left to right from FIG. 10E1, front view with flow from right to left and highlights the movements of the wings with light and dark shading.

FIGS. 10G1 through 10N1, forming a third sheet of related figures are intended to introduce further groups of direction of flow up in FIGS. 10G1, top view, left wing up, right wing down; FIG. 10H1, side view; FIG. 10K1, front view with direction of flow FIG. 10M1 showing a flow upward and per FIG. 10K1, Front view, a rotation of the wings clockwise. FIGS. 10I1 through Figure

FIGS. 10I1 through 10N1 show a second group of figures with the emphasis being that with a flow direction pointing down in FIG. 10N1, the same clockwise rotation seen in FIG. 10L1 results. FIG. 10I1 shows a top view with the left wing up while FIG. 10J1 shows a side view with the right wing down.

FIGS. 11A and 11B show two sets of counter-rotating fixed triangular (boomerang) wing turbines having one-way clutch bearings (OWCB's or Sprags) for turning the turbine in the same direction whether air/water flows from the left to right (FIG. 1A) or the right to the left (FIG. 11B). In FIG. 11A, the left turbine rotates clockwise because the left Sprag or one-way clutch bearing (OWCB) between the shaft and the wings is engaged. The right turbine rotates counterclockwise. As a result, the shaft rotates clockwise. Again, the emphasis is that the same clockwise rotation of the shaft results in FIG. 11 when the flow is from right to left. In FIG. 11B, the left turbine rotate counterclockwise and the right turbine rotates clockwise when the right sprag or one-way clutch bearing (OWCB) is engaged. Again, the left turbine rotates counterclockwise and the right turbine rotates clockwise but the shaft rotates in the same clockwise direction as in FIG. 11A.

Thus, there has been shown and described an improved concept for a harnessing module for a wind or water turbine that comprises pairs of concentric wings which may in alternative embodiments be triangular. Opposing concentric wings are lifted when water or wind flows and activates the circular side to lift or rotate the wing struck at an angle of attack greater than 0° and, for example, less than 50°. 

1. A harnessing module for harnessing renewable wind and water energy comprising opposing concentric wings for rotation about a turbine shaft having a hub, the harnessing module comprising: at least one pair of opposing concentric wings supported by a rotatable wing shaft for use in generating renewable electrical energy, each concentric wing of the opposing concentric wings having a circular side having a leading edge for facing one of air and water flow, having a generally flat surface but for a curved downward surface and a sharper side opposite the circular side of each concentric wing at a trailing edge, the circular side and a flat, curved upper surface being at a positive angle of attack with air or water flow where one of water or wind flow is received at the circular side leading edge of each concentric wing and provides lifting rotation of the opposing concentric wings; and the opposing concentric wings rotating about the shaft and comprise a harnessing module for generating electricity from either wind or water flow.
 2. The harnessing module of claim 1 comprising an increased number of opposing pairs of concentric wings where the number of opposing pairs is greater than or equal to two opposing pairs; the greater than or equal to two opposing pairs of concentric wings mounted to the same turbine shaft and hub, each opposing pair of concentric wings supported by a wing shaft and spaced equally about the hub, and the opposing pairs of concentric wings each having a wing support rotated by rack and pinion gears located in the hub.
 3. The harnessing module of claim 1 comprising an in-line harnessing module with high efficiency, the opposing pairs of concentric wings mounted on different hubs and mounted next to one another on the same turbine shaft
 4. The harnessing module of claim 1 comprising a minimum number of one pair of opposing concentric wings up to a maximum number of four pairs of opposing concentric wings comprising a set of opposing concentric wing pairs up to four opposing concentric wing pairs.
 5. The harnessing module of claim 4 comprising multiple pairs of concentric wings in a same plane, the multiple pairs of opposing wings in a same horizontal plane connected to the hub.
 6. The harnessing module of claim 4 comprising a multiple of four pairs of concentric wing pairs in three planes surrounding the shaft, the multiple sets of opposing concentric wings exhibiting the same direction of rotation upon engagement of a one way clutch bearing for one concentric wing pair, the engaged one-way clutch bearing located between a shaft and the one concentric wing pair.
 7. The harnessing module of claim 1 for receiving bi-directional flow of renewable energy, the angle of attack of each concentric wing being modified automatically by rack and pinion.
 8. The harnessing module of claim 7 for bi-directional flow, two turbines being assembled with multiple pairs of opposing concentric wings to a shaft which are contra-rotating, a one-way clutch bearing delivering a uni-directional rotation about the shaft.
 9. The harnessing module of claim 1 where a concentric wing comprises a triangular shape and an opposing pair of concentric wings of triangular shape have a wing shaft operable by rack and pinion.
 10. The harnessing module of claim 1 where a concentric wing comprises a boomerang shape with curved sides and an opposing pair of concentric wings of boomerang shape have a wing shaft operable by rack and pinion.
 11. A method of rotating a pair of rotating a concentric wing of an energy harnessing module from a first angle of attack of a leading edge by one of air and water and a second angle of attack, the concentric wing having a curved leading edge and a sharp trailing edge, the method of rotating comprising: moving a pinion circular gear positioned in a hub in one of an upward and a downward direction along a rack gear, the hub having a wing support shaft driven by the upward or downward movement of the pinion circular gear, the wing support shaft being located at an approximate center of a concentric wing between the curved leading edge and the sharp trailing edge of the concentric wing, and the wing support shaft rotating a concentric wing to a predetermined angle of attack by the one of air and water flow. 